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Ride qualities criteria validation/pilot performance study: Flight simulator resultsPilot performance was studied during simulated manual terrain following flight for ride quality criteria validation. An existing B-1 simulation program provided the data for these investigations. The B-1 simulation program included terrain following flights under varying controlled conditions of turbulence, terrain, mission length, and system dynamics. The flight simulator consisted of a moving base cockpit which reproduced motions due to turbulence and control inputs. The B-1 aircraft dynamics were programmed with six-degrees-of-freedom equations of motion with three symmetric and two antisymmetric structural degrees of freedom. The results provided preliminary validation of existing ride quality criteria and identified several ride quality/handling quality parameters which may be of value in future ride quality/criteria development.
Document ID
19760013737
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nardi, L. U.
(Rockwell International Corp. Los Angeles, CA, United States)
Kawana, H. Y.
(Rockwell International Corp. Los Angeles, CA, United States)
Borland, C. J.
(Rockwell International Corp. Los Angeles, CA, United States)
Lefritz, N. M.
(Rockwell International Corp. Los Angeles, CA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1976
Subject Category
Man/System Technology And Life Support
Report/Patent Number
H-936
NASA-CR-143838
Report Number: H-936
Report Number: NASA-CR-143838
Accession Number
76N20825
Funding Number(s)
CONTRACT_GRANT: NAS4-2236
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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